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aircraft:tmd:turbo_engines

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aircraft:tmd:turbo_engines [2021/02/12 13:14]
jh [Step 6 - Engine control (FADEC)]
aircraft:tmd:turbo_engines [2021/02/12 13:51] (current)
jh [Step 6 - Engine control (FADEC)]
Line 457: Line 457:
 Enrichment = Engine1Station3.OutputTotalPressure / ( PitotTube.StaticPressure * DesignCompressionRatio ). Enrichment = Engine1Station3.OutputTotalPressure / ( PitotTube.StaticPressure * DesignCompressionRatio ).
  
-FuelFlowRaw = C_FF * ( Governor + Enrichment )+Gain = PitotTube.StaticPressure / 101325.0 
 + 
 +FuelFlowRaw = Gain * C_FF * ( Governor + Enrichment )
  
 FuelFlow = clamp( FuelFlowRaw, MinFuelFlow, MaxFuelFlow )</code> FuelFlow = clamp( FuelFlowRaw, MinFuelFlow, MaxFuelFlow )</code>
aircraft/tmd/turbo_engines.txt · Last modified: 2021/02/12 13:51 by jh